JP2022525774A - 航空機の車輪の制動を制御するための方法、及び、関連する車輪制動制御装置 - Google Patents
航空機の車輪の制動を制御するための方法、及び、関連する車輪制動制御装置 Download PDFInfo
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- JP2022525774A JP2022525774A JP2021556262A JP2021556262A JP2022525774A JP 2022525774 A JP2022525774 A JP 2022525774A JP 2021556262 A JP2021556262 A JP 2021556262A JP 2021556262 A JP2021556262 A JP 2021556262A JP 2022525774 A JP2022525774 A JP 2022525774A
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- control device
- wheel braking
- thrust reverser
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- aircraft
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- 238000000034 method Methods 0.000 title claims description 12
- 230000005540 biological transmission Effects 0.000 claims description 2
- 230000003213 activating effect Effects 0.000 claims 1
- 238000012544 monitoring process Methods 0.000 claims 1
- 238000010586 diagram Methods 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 4
- 230000036461 convulsion Effects 0.000 description 3
- 230000001052 transient effect Effects 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 230000001627 detrimental effect Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000003044 adaptive effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000000306 recurrent effect Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
- B60T8/00—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force
- B60T8/17—Using electrical or electronic regulation means to control braking
- B60T8/1701—Braking or traction control means specially adapted for particular types of vehicles
- B60T8/1703—Braking or traction control means specially adapted for particular types of vehicles for aircrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/42—Arrangement or adaptation of brakes
- B64C25/426—Braking devices providing an automatic sequence of braking
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Regulating Braking Force (AREA)
Abstract
Description
Claims (10)
- 航空機の車輪の制動を監視するための方法において、
航空機の車輪の制動が、減速調整要求(16)及び逆推力装置展開要求(24)の両方に基づいて、前記航空機の車輪ブレーキ(10)を作動させる車輪制動制御装置(14)によって制御される、方法。 - 前記逆推力装置展開要求(24)は、前記航空機のコックピット(18)から前記車輪制動制御装置によって直接的に受けられる、請求項1に記載の方法。
- 前記車輪制動制御装置によって直接的に受けられた前記逆推力装置展開要求(24)は、逆推力装置(12)の展開を作動させる逆推力装置制御装置(22)に中継される、請求項2に記載の方法。
- 前記逆推力装置展開要求(24)は、前記逆推力装置制御装置(22)により直接的に受けられ、前記逆推力装置制御装置(22)は、前記逆推力装置展開要求(24)を車輪制動制御装置(14)に中継する、請求項1記載の方法。
- 前記逆推力装置(12)の展開によって生じた外乱を除去するために、前記逆推力装置の展開によって生じる外乱に比例した減速度設定値(36)の適合によって、前記車輪制動制御装置(14)によって前記車輪ブレーキ(10)に発される減速調整命令(20)が実質的に一定に保たれる、請求項1~4のいずれか1項に記載の方法。
- 前記逆推力装置(12)の展開によって生じた外乱を除去するために、前記逆推力装置の展開によって生じた前記外乱に比例して前記車輪制動調整ループの伝達関数におけるゲインの適合によって、前記車輪制動制御装置(14)によって前記車輪ブレーキ(10)に発せられる減速調整命令(20)が実質的に一定に保たれる、請求項1~4のいずれか1項に記載の方法。
- 前記逆推力装置の実際の状態に関する情報(30)が前記車輪制動制御装置(14)に送られる、請求項1~6のいずれか一項に記載の方法。
- 減速調整要求(16)に基づいて航空機の車輪のブレーキ(10)を作動させることができる車輪制動制御装置(14)において、
前記車輪制動制御装置(14)は、逆推力装置展開要求(24)にも基づいて航空機の車輪のブレーキ(10)を作動させるように構成されていることを特徴とする、車輪制動制御装置(14)。 - 前記車輪制動制御装置(14)は、前記逆推力装置の実際の状態に関する情報(30)を前記逆推力装置制御装置(22)から受けるようにさらに構成されていることを特徴とする、請求項8に記載の制御装置。
- 請求項8又は9に記載の車輪制動制御装置(14)を有する航空機。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1902924A FR3093993B1 (fr) | 2019-03-21 | 2019-03-21 | Procédé de contrôle du freinage des roues d’un avion et contrôleur de freinage de roues associé |
FR1902924 | 2019-03-21 | ||
PCT/FR2020/050541 WO2020188206A1 (fr) | 2019-03-21 | 2020-03-13 | Procede de controle du freinage des roues d'un avion et controleur de freinage de roues associe |
Publications (1)
Publication Number | Publication Date |
---|---|
JP2022525774A true JP2022525774A (ja) | 2022-05-19 |
Family
ID=67742588
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2021556262A Pending JP2022525774A (ja) | 2019-03-21 | 2020-03-13 | 航空機の車輪の制動を制御するための方法、及び、関連する車輪制動制御装置 |
Country Status (8)
Country | Link |
---|---|
US (1) | US11981312B2 (ja) |
EP (1) | EP3941825A1 (ja) |
JP (1) | JP2022525774A (ja) |
CN (1) | CN113544056A (ja) |
BR (1) | BR112021018327A2 (ja) |
CA (1) | CA3129015A1 (ja) |
FR (1) | FR3093993B1 (ja) |
WO (1) | WO2020188206A1 (ja) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112678154B (zh) * | 2021-01-11 | 2022-07-01 | 中南大学 | 一种具有干扰在线估计的飞机防滑刹车系统控制方法 |
Family Cites Families (21)
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FR1546878A (fr) * | 1966-11-29 | 1968-11-22 | Saab Ab | Dispositif pour régler la portance d'un avion pendant l'approche et pour inverser la poussée des réacteurs pendant le roulage au sol |
WO1994020344A1 (en) * | 1993-03-06 | 1994-09-15 | Dunlop Limited | Sequential selective operation of aircraft brakes |
US5539642A (en) * | 1993-05-21 | 1996-07-23 | The Boeing Company | Fuzzy logic autobrake system for aircraft |
US5505531A (en) * | 1995-05-12 | 1996-04-09 | The Boeing Company | Method to maintain brake stack closure during autobrake application |
US7720579B2 (en) * | 2006-12-20 | 2010-05-18 | The Boeing Company | Method, system, and computer program product for performance monitored aircraft rejected takeoff braking |
US8393689B2 (en) * | 2006-12-22 | 2013-03-12 | The Boeing Company | Autobraking interlock for an aircraft electric brake system |
FR2920196B1 (fr) * | 2007-08-20 | 2013-08-09 | Aircelle Sa | Inverseur de poussee avec systeme de freinage des actionneurs |
FR2930973B1 (fr) * | 2008-05-06 | 2010-04-23 | Airbus France | Procede et dispositif de mise en oeuvre des inverseurs de poussee d'un aeronef |
FR2941554B1 (fr) * | 2009-01-29 | 2011-04-01 | Airbus France | Procede et dispositif d'aide au pilotage d'un aeronef lors d'une phase d'atterrissage |
FR2943037B1 (fr) * | 2009-03-11 | 2012-09-21 | Airbus France | Systeme de commande d'aeronef a architecture modulaire integre. |
FR2978736B1 (fr) * | 2011-08-01 | 2013-09-27 | Airbus Operations Sas | Dispositif et procede de determination d'un etat de piste, aeronef comprenant un tel dispositif et systeme d'aide au pilotage exploitant cet etat de piste |
US9296488B2 (en) * | 2013-03-06 | 2016-03-29 | 3Rd Millennium Solutions, Inc. | Aircraft braking early warning system |
US9213334B2 (en) * | 2014-05-01 | 2015-12-15 | Goodrich Corporation | Runway traction estimation and reporting system |
DE102014210025A1 (de) * | 2014-05-26 | 2015-12-17 | Rolls-Royce Deutschland Ltd & Co Kg | Schubumkehrkaskadenelement einer Fluggasturbine |
FR3045563B1 (fr) * | 2015-12-18 | 2018-02-09 | Messier-Bugatti-Dowty | Procede et systeme de commande de freinage d’un aeronef equipe d’un systeme d’inversion de poussee |
US10815000B2 (en) * | 2016-05-31 | 2020-10-27 | Embraer S.A. | Short rejected takeoff system and method |
US9856035B1 (en) * | 2016-06-09 | 2018-01-02 | Goodrich Corporation | Systems and methods for dynamic light control |
US11037454B2 (en) * | 2016-11-03 | 2021-06-15 | The Boeing Company | Automatic braking system controller |
GB2563214A (en) * | 2017-06-05 | 2018-12-12 | Airbus Operations Ltd | Landing gear |
US20190054906A1 (en) * | 2017-08-18 | 2019-02-21 | Rockwell Collins, Inc. | Aircraft braking system and method using runway condition parameters |
US11186362B2 (en) * | 2018-12-17 | 2021-11-30 | The Boeing Company | Brake systems for aircraft and related methods |
-
2019
- 2019-03-21 FR FR1902924A patent/FR3093993B1/fr active Active
-
2020
- 2020-03-13 CN CN202080019250.3A patent/CN113544056A/zh active Pending
- 2020-03-13 JP JP2021556262A patent/JP2022525774A/ja active Pending
- 2020-03-13 US US17/436,263 patent/US11981312B2/en active Active
- 2020-03-13 BR BR112021018327A patent/BR112021018327A2/pt unknown
- 2020-03-13 CA CA3129015A patent/CA3129015A1/fr active Pending
- 2020-03-13 WO PCT/FR2020/050541 patent/WO2020188206A1/fr active Application Filing
- 2020-03-13 EP EP20726197.5A patent/EP3941825A1/fr active Pending
Also Published As
Publication number | Publication date |
---|---|
FR3093993A1 (fr) | 2020-09-25 |
EP3941825A1 (fr) | 2022-01-26 |
BR112021018327A2 (pt) | 2021-11-23 |
US11981312B2 (en) | 2024-05-14 |
FR3093993B1 (fr) | 2021-02-26 |
WO2020188206A1 (fr) | 2020-09-24 |
US20220169216A1 (en) | 2022-06-02 |
CN113544056A (zh) | 2021-10-22 |
CA3129015A1 (fr) | 2020-09-24 |
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